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<\/p>\nAirbus Defence and Space is in the home stretch of work to ship the first European Service Module (ESM) to its Florida launch site for integration with the rest of the hardware for NASA\u2019s Orion spacecraft. When fully assembled and tested, Orion will be launched on the Exploration Mission-1 (EM-1) test flight to orbit the Moon and return.\n<\/p>\n
ESM-1 is now undergoing subsystem functional testing at its Assembly, Integration, and Testing (AIT) facility in Bremen, Germany, following completion of most hardware that can be installed on-site. Also known as Flight Model-1 (FM-1), the module will be flown to the Kennedy Space Center this summer to begin the sequence of steps to put together the full Orion spacecraft.<\/p>\n
As FM-1 nears completion, Flight Model-2 (FM-2) has joined its sister module in the clean room at Bremen to begin its AIT flow. NASA and the European Space Agency (ESA) are also working with prime contractor Airbus on beginning construction of ESM hardware for subsequent modules this summer.<\/p>\n
FM-1 assembly nears completion, functional testing last major area of work<\/p>\n
The last stretch of work prior to the shipment of FM-1 is testing, following recent installations of its four large hypergolic propellant tanks and the Orbital Maneuvering System-E (OMS-E) main engine. \u201cThe main focus that we are working on is the functional testing of the propulsion subsystem and the consumable subsystem, meaning the water and oxygen for the astronauts,\u201d Bas Theelen, Airbus Vice President of the Orion ESM Programme, said in an interview.<\/p>\n
\u201cThat\u2019s really the big chunks of work still to be done, and then the shipment should be later this summer. We\u2019re almost done with all the hardware deliveries, so there\u2019s still one or two units to come but we have workarounds in place for those.\u201d<\/p>\n
\u201cThe integration \u2014 I don\u2019t know the percentage exactly \u2014 but it is largely complete,\u201d he added. \u201cWhat we still have here and there is, of course, small issues that you find, whether there is a heater that is disconnected or the wiring of a harness that is sometimes not right but nothing major.\u201d<\/p>\n
\u201cWe\u2019re working 24\/7, so we have teams in place basically all day in order to make sure that we get the maximum out of the time that we still have left to deliver.\u201d<\/p>\n
<\/p>\n
Airbus, ArianeGroup, and NASA personnel position the OMS-E engine (minus nozzle) for installation in FM-1, May 2018. Credit: Airbus Defence and Space<\/p>\n
The OMS-E main engine, minus its nozzle, was installed in the bottom of the module early in May. In addition, the Consumables Storage Subsystem (CSS) hardware, consisting of two groups of two gas tanks and two water tanks, was also recently installed in the top of the module.<\/p>\n
Installation of the propellant tanks in March and the OMS-E engine recently were major milestones in the AIT process for this first vehicle. \u201cThe reason why they are perceived as really big milestones is they are moments of no return,\u201d Theelen explained. \u201cIf you look at the design of the ESM, it is very densely packed. It is not like a telecom spacecraft or anything like that, that you more or less can fold out to exchange one of the units.\u201d<\/p>\n
\u201cOn the Orion ESM, the moment you install the tanks then everything behind it is no longer reachable,\u201d he continued, \u201cso the big milestones in the integration were indeed installation of the tanks and also of the Space Shuttle engine, because they represent moments that you say \u2018OK we are there, we have achieved what we needed to do\u2019 and now we can basically go to the next step that does not allow us to go back anymore.\u201d<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/ESM-Diagram.jpg\")
<\/p>\n
Diagram of the ESM highlighting upper module elements. Credit: Airbus Defence and Space<\/p>\n
The OMS-E engine was refurbished by NASA after use during the Space Shuttle program and provided to ESA and Airbus for the ESM. \u201cThe very fact that we have everything integrated implies therefore that the majority of the work is behind us,\u201d Theelen added.<\/p>\n
When shipped, the ESM will be missing its solar array wings and the nozzle of the OMS-E engine. The OMS-E nozzle is already in the United States and will be attached there. The solar generators will be shipped separately to the U.S.<\/p>\n
Installing the radiators around the outside of the module will be one of the final steps before shipment. \u201cThe moment you have those installed, you can\u2019t reach the hardware anymore,\u201d Theelen said. \u201cThe moment those are installed, then basically we\u2019re done.\u201d<\/p>\n
As the team in Bremen nears completion of FM-1, Theelen noted he had just had an all-hands meeting with them and continues to be impressed with their dedication. \u201cIt\u2019s very fascinating to see. I\u2019ve been in different programs before navigation, telecom, a bit of Earth observation as well,\u201d he noted.<\/p>\n
\u201cHuman spaceflight \u2014 I joined one and a half years ago \u2014 though, is different. The motivation and the commitment of the people is literally astounding, because of course we\u2019re on the critical path of the Orion program. We know that full well, so the pressure is high. At the same time, the motivation to continue, to every time give what it takes, [is high].\u201d<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/Orion_Earth_selife_DRO2_web.30pct.jpg\")
<\/p>\n
Orion takes a selfie from one of its solar array wing cameras from lunar orbit. Credit: Nathan Koga for NSF\/L2<\/p>\n
\u201cWe have our hurdles and setbacks, but people after swallowing, say \u2018OK, understood \u2014 we change this and we move on,\u2019 we continue. And that motivation is tangible in the team, also this morning again, and that\u2019s what I find pretty impressive.\u201d<\/p>\n
\u201cRecently I did speak with NASA in terms of what their opinion was in terms of the technical performance, the way we work, and there it\u2019s understood that we\u2019re doing everything we can to deliver, the quality of what we deliver is good, and the motivation of the people is much appreciated,\u201d he added.<\/p>\n
Subassembly functional testing ahead of full spacecraft integration and tests<\/p>\n
The ESM has multiple subsystems; in addition to the physical structure, there are subsystems covering propulsion, electrical power, thermal control, consumables, and avionics. The functional testing being done in Bremen now covers mainly the propulsion and consumables areas. Most of the other subsystems have more dependencies on equipment that Orion prime contractor Lockheed Martin is assembling in the crew module and crew module adapter that are being assembled in Florida.<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/ESM-Subsystems.jpg\")
<\/p>\n
Major subsystems of the ESM. Standalone testing in Bremen is focusing on the propulsion and consumable subsystems. Credit: Airbus Defence and Space<\/p>\n
\u201cWe\u2019ll test everything that we can do here,\u201d Theelen explained. \u201cThe number one subsystem is the propulsion subsystem and in reality you can say that the entire ESM design is built around the propulsion subsystem which itself is driven by the Space Shuttle engine. So we can test the entire propulsion subsystem here and that\u2019s the functional test that we\u2019re doing and there\u2019s no interruption\/interface between us and the crew module.\u201d<\/p>\n
\u201cWhen you look at the avionics subsystem, that\u2019s a different story. We don\u2019t have the onboard computer. That is the responsibility of Lockheed Martin, it\u2019s located in the crew module adapter. So that\u2019s one [where] we cannot do a full avionics subsystem test. Of course we can work with a simulator and we do that, but we cannot \u2014 to the fullest extent \u2014 test that one.\u201d<\/p>\n
\u201c[With] the power subsystem, we of course have the solar arrays, but we don\u2019t have the batteries,\u201d he continued. \u201cSo that implies that \u2014 if you\u2019re looking at a typical power subsystem \u2014 the battery you can of course to some extent simulate.\u201d<\/p>\n
\u201cFor the power subsystem here what we do have is the power control distribution unit (PCDU) for the ESM, so if you look at the solar array including of course the solar array drive mechanism, the solar array drive electronics and the PCDU, that\u2019s a pretty major part of the entire power subsystem, but it is not one-hundred percent complete.\u201d<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/ESM-CSS-Diagram.jpg\")
<\/p>\n
Diagram of the Consumable Storage System hardware. Credit: Airbus Defence and Space<\/p>\n
The CSS consists of four gas tanks that can be loaded with oxygen and nitrogen for crew cabin atmosphere and four water tanks. EM-1 is the first integrated flight for the Orion spacecraft, but it is an uncrewed test. To save some schedule time, Theelen noted that the ESM for this mission would only have one gas tank loaded with nitrogen and one loaded water tank. The others will be mass simulators.<\/p>\n
\u201cIf you go to the consumable subsystem, there again the entire subsystem is with us,\u201d he said. \u201cThere we can do the functional testing, at least for the part that we provide, but by definition of course when you look at the consumable subsystem there\u2019s of course an interface to the crew module and we don\u2019t have here an interface that represents the full functionality of each of those subsystems that interface with major functions that are inside the crew module.\u201d<\/p>\n
Shipment to Florida in the summer<\/p>\n
When the module is ready to go, it will be flown in a large cargo airlifter from Bremen to Florida. \u201cWe will ship with an Antonov, with a big container,\u201d Theelen noted. \u201cWe will also ship part of the ground support equipment of course because especially the electronics, the ground support equipment has to be in the U.S., as well.\u201d<\/p>\n
Airbus will have a support staff on-site in Florida and others remotely available. \u201cThere\u2019s about twenty [people on-site], but it depends on which phase of the testing we\u2019re in,\u201d he said.<\/p>\n
\u201c[Once] the ESM is shipped there, you get the normal unpacking procedures [and the] incoming inspection. Very soon afterwards there will be an integration readiness review with the crew module adapter in which the remainder of the power and avionics subsystems are located. There of course, we are present.\u201d<\/p>\n
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<\/p>\n
Orion service module elements with ESM center. The crew module adapter sits on top between the crew module and the ESM. The spacecraft adapter at the bottom attaches to the launch vehicle and provides space for the OMS-E nozzle. The Spacecraft Adapter Jettisoned (SAJ) panels are launch fairings. Credit: NASA<\/p>\n
\u201cThere will be moments of course where there will be dedicated tests for which we will have to fly in specialists on a case-by-case basis,\u201d he continued. \u201cThe moment you do the power subsystem testing for the entire spacecraft of course our people have to be there. The moment you do the functional testing of the propulsion subsystem together with the crew module, then of course our propulsion people will be there.\u201d<\/p>\n
\u201cWhen we start doing the overall spacecraft mechanical testing, vibration, etcetera, we will send our people in. So we will have a core team that will be there permanently and on a case-by-case basis we will have our specialists present.\u201d<\/p>\n
\u201cAnd then of course we have the normal back-office support of people here, by definition, that can always be asked for when needed. They will always be in Bremen, so there will always be the Bremen team in the background. There\u2019s a time zone difference, but you have to be there when anything happens and we\u2019ll be there on-site.\u201d<\/p>\n
At KSC, the ESM will first be attached to the crew module adapter and checked out before the crew module is brought in to be integrated.<\/p>\n
FM-2 AIT underway, building on lessons learned<\/p>\n
While work in Bremen on the first ESM is nearing completion, the structure for the second unit has moved into the same clean room. Built by Thales Alenia Espace in Turin, Italy, the structure was transported to Bremen in late April, and is now beginning its AIT flow for eventual service on Exploration Mission-2 (EM-2), the first crewed Orion flight.<\/p>\n
\u201cOn the lower level, the normal preparation, all the work has started,\u201d Theelen said. \u201cWe\u2019re waiting for the other major deliveries and some of them we haven\u2019t received yet, but you can do all the bracket mounting, the harness mounting, all that kind of preparation.\u201d<\/p>\n
\u201cThere\u2019s about 11000 meters of cables in there, so there\u2019s a lot of work that you can prepare already, especially now that you have [that work on] FM-1 already behind.\u201d<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/ESM-FM-2-Structure-Composite.jpg\")
<\/p>\n
Images of the FM-2 structure. On the left, being prepared at Thales Alenia Espace in Turin; on the right in the Airbus clean room in Bremen. Credit: Airbus Defence and Space<\/p>\n
Lessons learned during the first AIT flow are being incorporated by the team as they go. \u201cBasically I\u2019ve only got one team, I don\u2019t have two teams,\u201d Theelen explained. \u201cThe AIT manager for the second one is sitting the same office, sitting right next to the AIT manager for ESM-1. So there\u2019s one thing.\u201d<\/p>\n
\u201cThe other thing is, if you look at the lessons learned, and of course as we go we discover stuff that we didn\u2019t expect or things don\u2019t go exactly as planned, those are being captured in a special lessons learned database to make sure that they are available and used for ESM-2.\u201d<\/p>\n
Theelen noted, though, that the design drives the sequence of events in the flow. \u201cThe particular thing about the entire ESM is \u2014 and I come back to that \u2014 the design is such that it is extremely compact,\u201d he explained.<\/p>\n
\u201cThe design is driven by the fact that we have one OMS-E engine in the middle, and the structural design and the thermal design have developed such that you have the central core section and you have the six compartments around it. This design implies that there\u2019s also only a limited number of ways that you can integrate ESM. It\u2019s not fully up to you, how to integrate it \u2014 it has to be in a specific order.\u201d<\/p>\n
He continued, noting that deliveries of major hardware for FM-2 will be one key to the pace of processing. \u201cTo some extent the AIT flow is driven by when which unit arrives,\u201d he explained. \u201cAnd on ESM-1, when which unit arrives is different than on ESM-2.\u201d<\/p>\n
\u201cSo to some extent the AIT flow is also driven or changed by means of the availability of the equipment that you mount, and the best example is the [propellant] tank. The moment you put the tank in, that\u2019s the propellant tank, that\u2019s the moment of no return for quite a bit of the work. So if that would come really, really late, then of course work is halted.\u201d<\/p>\n
\u201cThe good thing about it is that since we have done ESM-1, we have done quite a few workarounds in that case. So we know today that in case something comes late for whatever reason, we have the workaround ready now, because we have experienced it on ESM-1,\u201d he added.<\/p>\n
\u201cSo beyond that, there\u2019s also a lot of optimization of repetitive work \u2014 in the engines we have, I don\u2019t know how many brackets we have, there\u2019s hundreds of them. We have 11 kilometers of cable inside, so from there, there are generic lessons learned on how to optimize the process of the steps that we make before integration. So that\u2019s a couple of typical lessons learned.\u201d<\/p>\n
Theelen also noted a positive lesson learned: \u201cThe concurrent way of working in which the design evolves and is finalized and there are several models that you need in advance, whether that\u2019s structural or functional, that\u2019s an approach that works. It comes with workarounds, because there is always uncertainty but so far that has proven to work, which is a big relief.\u201d<\/p>\n
\u201cI mean, let\u2019s face it \u2014 we haven\u2019t delivered yet, so there\u2019s always a risk, but that is a lesson learned,\u201d he added. \u201cAt the beginning of the program people were wondering \u2018is this all going to work?\u2019 and so far the answer is yes.\u201d<\/p>\n
PQM testing on hold due to anomaly last year<\/p>\n
While the AIT work progresses on the flight units, Orion development work continues with structural and functional models. Testing of the Propulsion Qualification Module (PQM) began last year at White Sands, but an anomaly occurred that suspended testing.<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/orion-esm-firing-tests-oms-e.jpg\")
<\/p>\n
Test-firing of one of the PQM\u2019s eight Auxiliary engines at White Sands in 2017. Credit: Airbus Defence and Space<\/p>\n
\u201cDuring testing of the PQM at White Sands, one of the system\u2019s Reaction Control System thrusters experienced a failure during blow down testing last August,\u201d NASA said in a statement provided by Rachel Kraft with Johnson Space Center Public Affairs.<\/p>\n
\u201cThe testing was stopped immediately and no one was injured. NASA and its partners formed a team to investigate what caused the anomaly and assessed impacts to the schedule of testing planned for the system. Blow down testing, which does not involve active pressure regulation of the propellant tanks, is done to provide data that can be compared to later tests involving active propellant tank pressure regulation.\u201d<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/oms-e-second-firing-1024x923.jpg\")
<\/p>\n
Test-firing of OMS-E engine on the PQM at White Sands in 2017. Credit: Airbus Defence and Space<\/p>\n
\u201cWe stopped testing and we have been taking some time to come to a clear definition of the root cause,\u201d Theelen added. \u201cEven though it has not been a hundred percent unambiguously identified, it\u2019s been pretty clear what the workarounds are that are necessary to prevent it in the future.\u201d<\/p>\n
\u201cThere was a number of minor improvements of the propulsion system design, but that was also covered relatively quickly,\u201d he noted. \u201cIf we would have had a major problem, then we would have had a major redesign and that is not something that you fix in a matter of months.\u201d<\/p>\n
\u201cSo there has been an agreement between all the parties \u2014 NASA, ESA, Aerojet, Ariane Group, [and] ourselves \u2014 on the way forward on that one. We have done some refurbishment of the RCS thrusters that have been implemented and we now are back in White Sands at this moment for the preparation of continuation of testing that should start now in August.\u201d<\/p>\n
Plans for FM-3 and beyond<\/p>\n
NASA, ESA, and Airbus also continue to lay the groundwork for construction of future ESM flight models.<\/p>\n
\u201cAs the mission requirements from NASA mature, there have been some requests for improvements of performance, especially on the propulsion side,\u201d Theelen explained. \u201cSo there\u2019s been a study phase until the Systems Requirements Review to see, OK now what needs to be done, improved [in] the propulsion subsystem. The other thing is that because of the mission scenario being slightly different, the load cases on for example the solar arrays are slightly different.\u201d<\/p>\n
\u201cSo that is done in a normal study phase,\u201d he continued. \u201cThen at the same time it has become clear that some of the changes that are necessary will take quite a bit of time, so some of those design changes will be implemented only on the fourth module, whereas the third one will be largely a recurring one of ESM-2.\u201d<\/p>\n
\u201cSo the Systems Requirements Review also concluded on which changes are going to be implemented on number three and which changes only are going to be implemented on number four. And now, just like with any program we are negotiating with ESA on the price on ESM-3 and 4. Expectations are that we would start work already on three and four this summer.\u201d<\/p>\n","protected":false},"excerpt":{"rendered":"
Airbus Defence and Space is in the home stretch of work to ship the first European Service Module (ESM) to its Florida launch site for integration with the rest of the hardware for NASA\u2019s Orion spacecraft. When fully assembled and tested, Orion will be launched on the Exploration Mission-1 (EM-1) test flight to orbit the […]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[8394,640],"class_list":["post-38411","post","type-post","status-publish","format-standard","hentry","category-news","tag-esm","tag-orion"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/38411"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=38411"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/38411\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=38411"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=38411"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=38411"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}